FR2861690B1 - ATTITUDE CONTROL OF SATELLITES IN PARTICULAR AGILES WITH REDUCED NUMBER OF GYRODYNES - Google Patents
ATTITUDE CONTROL OF SATELLITES IN PARTICULAR AGILES WITH REDUCED NUMBER OF GYRODYNESInfo
- Publication number
- FR2861690B1 FR2861690B1 FR0312914A FR0312914A FR2861690B1 FR 2861690 B1 FR2861690 B1 FR 2861690B1 FR 0312914 A FR0312914 A FR 0312914A FR 0312914 A FR0312914 A FR 0312914A FR 2861690 B1 FR2861690 B1 FR 2861690B1
- Authority
- FR
- France
- Prior art keywords
- agiles
- gyrodynes
- satellites
- reduced number
- attitude control
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/244—Spacecraft control systems
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0312914A FR2861690B1 (en) | 2003-11-04 | 2003-11-04 | ATTITUDE CONTROL OF SATELLITES IN PARTICULAR AGILES WITH REDUCED NUMBER OF GYRODYNES |
PCT/FR2004/002800 WO2005045366A1 (en) | 2003-11-04 | 2004-10-29 | Method of controlling the attitude of satellites, particularly agile satellites with a reduced number of gyrodynes |
EP04805353A EP1680648B1 (en) | 2003-11-04 | 2004-10-29 | Method of controlling the attitude of satellites, particularly agile satellites with a reduced number of control moment gyroscopes |
US10/595,621 US7661627B2 (en) | 2003-11-04 | 2004-10-29 | Method of controlling the attitude of satellites, particularly agile satellites with a reduced number of gyrodynes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0312914A FR2861690B1 (en) | 2003-11-04 | 2003-11-04 | ATTITUDE CONTROL OF SATELLITES IN PARTICULAR AGILES WITH REDUCED NUMBER OF GYRODYNES |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2861690A1 FR2861690A1 (en) | 2005-05-06 |
FR2861690B1 true FR2861690B1 (en) | 2006-04-07 |
Family
ID=34429871
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR0312914A Expired - Fee Related FR2861690B1 (en) | 2003-11-04 | 2003-11-04 | ATTITUDE CONTROL OF SATELLITES IN PARTICULAR AGILES WITH REDUCED NUMBER OF GYRODYNES |
Country Status (4)
Country | Link |
---|---|
US (1) | US7661627B2 (en) |
EP (1) | EP1680648B1 (en) |
FR (1) | FR2861690B1 (en) |
WO (1) | WO2005045366A1 (en) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US7805226B2 (en) * | 2006-09-29 | 2010-09-28 | Honeywell International Inc. | Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes |
FR2937954B1 (en) * | 2008-10-31 | 2011-07-29 | Thales Sa | METHOD AND SYSTEM FOR DESATURING INERTIAL WHEELS OF A SPATIAL GEAR |
US8209070B2 (en) * | 2008-12-17 | 2012-06-26 | Honeywell International Inc. | Methods and systems for efficiently orienting an agile vehicle using a gyroscope array |
US8312782B2 (en) * | 2009-06-18 | 2012-11-20 | Honeywell International Inc. | Control moment gyroscope based momentum control systems in small satellites |
CN102749924B (en) * | 2012-06-18 | 2015-02-11 | 北京控制工程研究所 | Method for identifying reconfigurable weak link of satellite control system |
FR2993863B1 (en) * | 2012-07-27 | 2014-08-29 | Thales Sa | METHOD FOR REDUCING THE KINETIC MOMENT AND ATTITUDE CONTROL OF A SPATIAL MACHINE |
CN103708044B (en) * | 2013-12-06 | 2016-02-10 | 上海新跃仪表厂 | A kind of saturated sliding mode variable structure control method for satellite rapid attitude maneuver |
US10202208B1 (en) | 2014-01-24 | 2019-02-12 | Arrowhead Center, Inc. | High control authority variable speed control moment gyroscopes |
US9511882B2 (en) * | 2014-05-16 | 2016-12-06 | Honeywell International Inc. | Configurable space station momentum |
CN107850900A (en) | 2015-06-02 | 2018-03-27 | 查尔斯斯塔克德雷珀实验室有限公司 | Quick rotation and installing system for grapefruit satellite |
US10005568B2 (en) | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
FR3046686B1 (en) * | 2016-01-08 | 2019-10-18 | Centre National D'etudes Spatiales (Cnes) | DEVICE FOR CONTROLLING THE ATTITUDE OF A SPACE DEVICE |
US10175065B2 (en) | 2016-02-02 | 2019-01-08 | Honeywell International Inc. | Near-zero revolutions per minute (RPM) sensing |
US11221633B2 (en) * | 2016-05-17 | 2022-01-11 | Raytheon Company | Gyroscopic attitude control system |
CN113311878A (en) | 2016-05-31 | 2021-08-27 | 深圳市大疆灵眸科技有限公司 | Method and system for adaptive pan-tilt |
CN107152926B (en) * | 2016-07-18 | 2018-08-24 | 哈尔滨工业大学 | A kind of satellite quickly rotates super large breadth sweeping imaging method |
CN107466385B (en) * | 2016-08-03 | 2021-06-01 | 深圳市大疆灵眸科技有限公司 | Cloud deck control method and system |
JP6681805B2 (en) * | 2016-08-19 | 2020-04-15 | 三菱電機株式会社 | Attitude control device, spacecraft, attitude control method, and attitude control program |
US10175700B2 (en) * | 2017-03-22 | 2019-01-08 | The Boeing Company | Methods and apparatus to minimize command dynamics of a satellite |
US10732586B2 (en) * | 2017-07-12 | 2020-08-04 | X Development Llc | Active disturbance compensation for physically changing systems |
CN107628273B (en) * | 2017-09-27 | 2019-06-04 | 上海航天控制技术研究所 | A kind of satellite attitude control method based on the variable control period |
FR3094479B1 (en) * | 2019-03-25 | 2021-08-27 | Airbus Defence & Space Sas | Device and method for determining the attitude of a satellite equipped with gyroscopic actuators, and a satellite carrying such a device |
CN111595309A (en) * | 2020-04-24 | 2020-08-28 | 中电投电力工程有限公司 | System and method for improving verticality measurement precision by using multiple micro-mechanical gyroscopes |
CN111966103B (en) * | 2020-08-18 | 2021-04-20 | 国以贤智能科技(上海)股份有限公司 | Method, device, equipment and medium for dynamically correcting zero deflection angle of unmanned forklift |
CN114115305B (en) * | 2021-11-01 | 2022-10-04 | 武汉大学 | Control system design method of high-precision remote sensing small satellite with quick attitude maneuvering |
CN114212278B (en) * | 2021-11-29 | 2023-11-14 | 上海航天控制技术研究所 | Satellite stability control and interference compensation method |
CN116499444B (en) * | 2023-06-20 | 2023-09-05 | 中国船舶集团有限公司第七〇七研究所 | Hemispherical resonant gyro mode switching method based on vibration mode active precession |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5681012A (en) | 1995-01-05 | 1997-10-28 | Hughes Electronics | Spacecraft control with skewed control moment gyros |
FR2786283B1 (en) * | 1998-11-19 | 2001-01-26 | Matra Marconi Space France | METHOD AND DEVICE FOR CONTROLLING THE ATTITUDE OF A SATELLITE |
US6241194B1 (en) * | 1999-06-28 | 2001-06-05 | Honeywell International Inc. | Momentum position control |
US6360996B1 (en) | 2000-02-24 | 2002-03-26 | Hughes Electronics Corporation | Steering control for skewed scissors pair CMG clusters |
-
2003
- 2003-11-04 FR FR0312914A patent/FR2861690B1/en not_active Expired - Fee Related
-
2004
- 2004-10-29 WO PCT/FR2004/002800 patent/WO2005045366A1/en active Application Filing
- 2004-10-29 US US10/595,621 patent/US7661627B2/en not_active Expired - Fee Related
- 2004-10-29 EP EP04805353A patent/EP1680648B1/en active Active
Also Published As
Publication number | Publication date |
---|---|
US20080035797A1 (en) | 2008-02-14 |
FR2861690A1 (en) | 2005-05-06 |
WO2005045366A1 (en) | 2005-05-19 |
US7661627B2 (en) | 2010-02-16 |
EP1680648B1 (en) | 2012-07-25 |
EP1680648A1 (en) | 2006-07-19 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
CA | Change of address | ||
PLFP | Fee payment |
Year of fee payment: 13 |
|
PLFP | Fee payment |
Year of fee payment: 14 |
|
PLFP | Fee payment |
Year of fee payment: 15 |
|
PLFP | Fee payment |
Year of fee payment: 16 |
|
PLFP | Fee payment |
Year of fee payment: 17 |
|
ST | Notification of lapse |
Effective date: 20210705 |